Date:
June 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2008/171/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -383823
34 A = 6718501
49 meter
Y = 4155376
16 meter E =
0006405
Z = 5270827
92 I = 51
63847
XDOT = -7674
093384 Wp = 270
38447
YDOT = -594
099612 meter/sec RA = 3
89352 deg
ZDOT = -90
510149 TA = 180
47445
MA = 180
47506
Ha = 187
029 n
mi
Hp = 186
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1259262
93 X = -455865
54
Y = 13633123
88 feet Y = 4150680
07 meter
Z = 17292742
52 Z = 5268789
23
XDOT = -25177
471732 XDOT = -7666
440032
YDOT = -1949
145708 feet/sec YDOT = -679
872905 meter/sec
ZDOT = -296
949307 ZDOT = -127
772340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13682642
06 X = 4170469
30
Y = 702662
92 feet Y = 214171
66 meter
Z = 17285205
38 Z = 5268530
60
XDOT = -688
706368 XDOT = -209
917701
YDOT = 24242
113161 feet/sec YDOT = 7388
996092 meter/sec
ZDOT = -440
473066 ZDOT = -134
256190
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08171
56237797
00020000 00000-0 20000-3 0 9002
2 25544 51
6371 4
1419 0008792 268
9936 91
0220 15
74564316 28908
Satellite: ISS
Catalog Number: 25544
Epoch time: 08171
56237797 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 4
1419 deg
Eccentricity:
0008792
Arg of perigee: 268
9936 deg
Mean anomaly: 91
0220 deg
Mean motion: 15
74564316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2890
Checksum: 302
Coasting Arc #2 (Orbit 2905)
---------------------------------------
Vector Time (GMT): 2008/172/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6716799
38 A = 6730364
77 meter
Y = 94634
90 meter E =
0008966
Z = 303805
32 I = 51
64922
XDOT = -340
288026 Wp = 4
76959
YDOT = 4779
848924 meter/sec RA = 358
75657 deg
ZDOT = 6030
566461 TA = 358
53310
MA = 358
53573
Ha = 187
150 n
mi
Hp = 186
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22036743
38 X = 6713766
13
Y = 310481
95 feet Y = 169728
97 meter
Z = 996736
61 Z = 336427
98
XDOT = -1116
430532 XDOT = -423
006966
YDOT = 15681
919043 feet/sec YDOT = 4775
579858 meter/sec
ZDOT = 19785
323034 ZDOT = 6028
713432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1124735
54 X = -342819
39
Y = -22004163
51 feet Y = -6706869
04 meter
Z = 1122363
44 Z = 342096
38
XDOT = 14124
220261 XDOT = 4305
062336
YDOT = 287
467964 feet/sec YDOT = 87
620235 meter/sec
ZDOT = 19778
548727 ZDOT = 6028
501652
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08172
57781165
00020000 00000-0 20000-3 0 9018
2 25544 51
6366 358
9208 0008861 272
8755 87
1394 15
74622096 29064
Satellite: ISS
Catalog Number: 25544
Epoch time: 08172
57781165 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 358
9208 deg
Eccentricity:
0008861
Arg of perigee: 272
8755 deg
Mean anomaly: 87
1394 deg
Mean motion: 15
74622096 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2906
Checksum: 324
Coasting Arc #3 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2008/173/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 216268
59 A = 6718367
12 meter
Y = -4206112
66 meter E =
0006123
Z = -5239611
86 I = 51
57990
XDOT = 7664
517556 Wp = 93
11381
YDOT = -369
502558 meter/sec RA = 353
60552 deg
ZDOT = 613
264657 TA = 182
72065
MA = 182
72399
Ha = 187
331 n
mi
Hp = 186
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 709542
60 X = 288738
78
Y = -13799582
21 feet Y = -4203288
00 meter
Z = -17190327
61 Z = -5238386
02
XDOT = 25146
054975 XDOT = 7665
100649
YDOT = -1212
278733 feet/sec YDOT = -283
790392 meter/sec
ZDOT = 2012
023153 ZDOT = 650
499894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13819332
22 X = -4212132
46
Y = 330510
71 feet Y = 100739
67 meter
Z = -17185927
47 Z = -5238270
69
XDOT = -3251
889994 XDOT = -991
176070
YDOT = -23941
509869 feet/sec YDOT = -7297
372208 meter/sec
ZDOT = 2155
381055 ZDOT = 656
960145
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08173
52976586
00020000 00000-0 20000-3 0 9028
2 25544 51
6366 354
0269 0008716 276
2201 83
7969 15
74657540 29210
Satellite: ISS
Catalog Number: 25544
Epoch time: 08173
52976586 = yrday
fracday
Element set: 902
Inclination: 51
6366 deg
RA of node: 354
0269 deg
Eccentricity:
0008716
Arg of perigee: 276
2201 deg
Mean anomaly: 83
7969 deg
Mean motion: 15
74657540 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2921
Checksum: 320
Coasting Arc #4 (Orbit 2936)
---------------------------------------
Vector Time (GMT): 2008/174/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6640925
69 A = 6729829
50 meter
Y = 725463
27 meter E =
0006571
Z = -777042
53 I = 51
59067
XDOT = 167
913607 Wp = 198
36648
YDOT = -4863
707210 meter/sec RA = 348
47421 deg
ZDOT = -5968
402366 TA = 350
11244
MA = 350
12536
Ha = 187
567 n
mi
Hp = 186
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21787813
93 X = -6644769
67
Y = 2380128
84 feet Y = 651179
28 meter
Z = -2549352
14 Z = -809313
04
XDOT = 550
897660 XDOT = 251
280987
YDOT = -15957
044653 feet/sec YDOT = -4861
362340 meter/sec
ZDOT = -19581
372593 ZDOT = -5967
384995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4532612
99 X = 1381540
44
Y = 21428497
53 feet Y = 6531406
05 meter
Z = -2673566
64 Z = -814903
11
XDOT = -14381
384733 XDOT = -4383
446066
YDOT = 596
390707 feet/sec YDOT = 181
779888 meter/sec
ZDOT = -19577
829098 ZDOT = -5967
322309
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08174
54516565
00020000 00000-0 20000-3 0 9039
2 25544 51
6370 348
8067 0008835 281
9229 78
0943 15
74724051 29375
Satellite: ISS
Catalog Number: 25544
Epoch time: 08174
54516565 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 348
8067 deg
Eccentricity:
0008835
Arg of perigee: 281
9229 deg
Mean anomaly: 78
0943 deg
Mean motion: 15
74724051 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2937
Checksum: 316
Coasting Arc #5 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2008/175/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -78417
30 A = 6718705
83 meter
Y = 4306291
25 meter E =
0006716
Z = 5161726
02 I = 51
52370
XDOT = -7500
290777 Wp = 310
90037
YDOT = 1274
734170 meter/sec RA = 343
30909 deg
ZDOT = -1174
089298 TA = 150
35309
MA = 150
31500
Ha = 187
770 n
mi
Hp = 186
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -257274
59 X = -151639
59
Y = 14128252
14 feet Y = 4305004
16 meter
Z = 16934796
65 Z = 5161167
87
XDOT = -24607
253207 XDOT = -7508
284161
YDOT = 4182
198720 feet/sec YDOT = 1190
817106 meter/sec
ZDOT = -3851
999008 ZDOT = -1210
544594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14073351
26 X = 4289557
46
Y = -1294573
60 feet Y = -394586
03 meter
Z = 16932982
60 Z = 5161173
10
XDOT = 6923
536558 XDOT = 2110
293943
YDOT = 22903
982464 feet/sec YDOT = 6981
133855 meter/sec
ZDOT = -3992
286145 ZDOT = -1216
848817
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08175
56055174
00020000 00000-0 20000-3 0 9047
2 25544 51
6367 343
5859 0008650 284
3491 75
6712 15
74663163 29536
Satellite: ISS
Catalog Number: 25544
Epoch time: 08175
56055174 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 343
5859 deg
Eccentricity:
0008650
Arg of perigee: 284
3491 deg
Mean anomaly: 75
6712 deg
Mean motion: 15
74663163 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2953
Checksum: 315
Coasting Arc #6 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2008/176/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6431422
96 A = 6729300
53 meter
Y = -1480390
04 meter E =
0010418
Z = 1278681
68 I = 51
53361
XDOT = -10
696340 Wp = 20
53990
YDOT = 5011
747062 meter/sec RA = 338
18258 deg
ZDOT = 5851
378322 TA = 353
52011
MA = 353
53357
Ha = 187
757 n
mi
Hp = 185
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21100469
03 X = 6441287
36
Y = -4856922
70 feet Y = -1408415
20 meter
Z = 4195149
86 Z = 1309949
09
XDOT = -35
092980 XDOT = -95
162436
YDOT = 16442
739705 feet/sec YDOT = 5011
154392 meter/sec
ZDOT = 19197
435438 ZDOT = 5851
121863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7628550
02 X = -2325182
05
Y = -20238600
97 feet Y = -6168725
58 meter
Z = 4315440
76 Z = 1315346
34
XDOT = 14838
982724 XDOT = 4522
921934
YDOT = -1496
724548 feet/sec YDOT = -456
201642 meter/sec
ZDOT = 19196
842275 ZDOT = 5851
197526
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08176
57591611
00020000 00000-0 20000-3 0 9051
2 25544 51
6376 338
3654 0008730 287
8330 72
1881 15
74749612 29690
Satellite: ISS
Catalog Number: 25544
Epoch time: 08176
57591611 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 338
3654 deg
Eccentricity:
0008730
Arg of perigee: 287
8330 deg
Mean anomaly: 72
1881 deg
Mean motion: 15
74749612 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2969
Checksum: 323
Coasting Arc #7 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2008/177/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -69516
65 A = 6718988
24 meter
Y = -4459071
34 meter E =
0004950
Z = -5029807
73 I = 51
47270
XDOT = 7196
480117 Wp = 88
14078
YDOT = -2094
300076 meter/sec RA = 333
00533 deg
ZDOT = 1758
840766 TA = 198
82982
MA = 198
84814
Ha = 187
978 n
mi
Hp = 185
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -228072
99 X = 4784
39
Y = -14629499
14 feet Y = -4459432
65 meter
Z = -16501993
86 Z = -5029965
52
XDOT = 23610
499073 XDOT = 7210
819947
YDOT = -6871
063242 feet/sec YDOT = -2013
744951 meter/sec
ZDOT = 5770
474955 ZDOT = 1793
835751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14442555
38 X = -4402090
88
Y = 2335620
50 feet Y = 711897
13 meter
Z = -16502955
33 Z = -5030100
78
XDOT = -10173
045475 XDOT = -3100
744261
YDOT = -21220
372466 feet/sec YDOT = -6467
969528 meter/sec
ZDOT = 5905
068482 ZDOT = 1799
864873
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08177
52780658
00020000 00000-0 20000-3 0 9069
2 25544 51
6381 333
4722 0008681 292
0191 68
0050 15
74764790 29849
Satellite: ISS
Catalog Number: 25544
Epoch time: 08177
52780658 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 333
4722 deg
Eccentricity:
0008681
Arg of perigee: 292
0191 deg
Mean anomaly: 68
0050 deg
Mean motion: 15
74764790 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2984
Checksum: 310
Coasting Arc #8 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2008/178/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6115388
31 A = 6728411
22 meter
Y = 2144625
21 meter E =
0003765
Z = -1802453
20 I = 51
47916
XDOT = -159
931484 Wp = 242
15072
YDOT = -5218
023942 meter/sec RA = 327
88316 deg
ZDOT = -5658
725547 TA = 317
87823
MA = 317
90716
Ha = 188
208 n
mi
Hp = 185
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20063609
93 X = -6130159
32
Y = 7036171
96 feet Y = 2076157
07 meter
Z = -5913560
38 Z = -1832197
44
XDOT = -524
709592 XDOT = -74
081708
YDOT = -17119
501122 feet/sec YDOT = -5219
331669 meter/sec
ZDOT = -18565
372528 ZDOT = -5659
294619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10293219
16 X = 3137373
20
Y = 18567177
67 feet Y = 5659275
75 meter
Z = -6027927
36 Z = -1837312
26
XDOT = -15453
364828 XDOT = -4710
185600
YDOT = 2531
225007 feet/sec YDOT = 771
517382 meter/sec
ZDOT = -18567
979674 ZDOT = -5659
520205
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08178
54313804
00020000 00000-0 20000-3 0 9078
2 25544 51
6377 328
2510 0008793 296
8946 63
1318 15
74807460 30000
Satellite: ISS
Catalog Number: 25544
Epoch time: 08178
54313804 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 328
2510 deg
Eccentricity:
0008793
Arg of perigee: 296
8946 deg
Mean anomaly: 63
1318 deg
Mean motion: 15
74807460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3000
Checksum: 300
Coasting Arc #9 (Orbit 3015)
---------------------------------------
Vector Time (GMT): 2008/179/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 224199
02 A = 6719817
11 meter
Y = 4671629
39 meter E =
0008112
Z = 4829369
29 I = 51
42592
XDOT = -6774
093130 Wp = 348
94493
YDOT = 2784
048854 meter/sec RA = 322
69221 deg
ZDOT = -2371
448504 TA = 124
29872
MA = 124
22190
Ha = 188
408 n
mi
Hp = 185
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 735561
09 X = 148483
11
Y = 15326868
08 feet Y = 4673712
50 meter
Z = 15844387
44 Z = 4830275
18
XDOT = -22224
714995 XDOT = -6793
201200
YDOT = 9134
018550 feet/sec YDOT = 2708
190550 meter/sec
ZDOT = -7780
342861 ZDOT = -2404
403288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14944735
07 X = 4555155
25
Y = -3462148
84 feet Y = -1055262
97 meter
Z = 15848248
09 Z = 4830546
02
XDOT = 12817
212734 XDOT = 3906
686441
YDOT = 19024
003152 feet/sec YDOT = 5798
516161 meter/sec
ZDOT = -7907
020538 ZDOT = -2410
059860
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08179
55845414
00020000 00000-0 20000-3 0 9088
2 25544 51
6381 323
0304 0008671 300
5209 59
5098 15
74777683 30163
Satellite: ISS
Catalog Number: 25544
Epoch time: 08179
55845414 = yrday
fracday
Element set: 908
Inclination: 51
6381 deg
RA of node: 323
0304 deg
Eccentricity:
0008671
Arg of perigee: 300
5209 deg
Mean anomaly: 59
5098 deg
Mean motion: 15
74777683 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3016
Checksum: 303
Coasting Arc #10 (Orbit 3031)
---------------------------------------
Vector Time (GMT): 2008/180/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5700119
49 A = 6727247
88 meter
Y = -2683415
60 meter E =
0010694
Z = 2338362
35 I = 51
43063
XDOT = 369
942732 Wp = 34
25995
YDOT = 5489
713592 meter/sec RA = 317
57503 deg
ZDOT = 5394
769389 TA = 352
16661
MA = 352
18330
Ha = 188
351 n
mi
Hp = 184
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18701179
44 X = 5718342
78
Y = -8803856
95 feet Y = -2619572
08 meter
Z = 7671792
48 Z = 2366097
61
XDOT = 1213
722873 XDOT = 282
321351
YDOT = 18010
871365 feet/sec YDOT = 5493
359718 meter/sec
ZDOT = 17699
374636 ZDOT = 5396
354637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12380848
37 X = -3773682
58
Y = -16501811
91 feet Y = -5029752
27 meter
Z = 7778380
73 Z = 2370850
45
XDOT = 16214
496339 XDOT = 4942
178484
YDOT = -3814
412416 feet/sec YDOT = -1162
632904 meter/sec
ZDOT = 17705
914940 ZDOT = 5396
762874
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08180
57374820
00020000 00000-0 20000-3 0 9091
2 25544 51
6392 317
8095 0008804 303
9788 56
0538 15
74874851 30324
Satellite: ISS
Catalog Number: 25544
Epoch time: 08180
57374820 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 317
8095 deg
Eccentricity:
0008804
Arg of perigee: 303
9788 deg
Mean anomaly: 56
0538 deg
Mean motion: 15
74874851 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3032
Checksum: 317
Coasting Arc #11 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2008/181/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -446179
71 A = 6720631
80 meter
Y = -4916448
47 meter E =
0003347
Z = -4561617
75 I = 51
38741
XDOT = 6267
098570 Wp = 53
12441
YDOT = -3333
917356 meter/sec RA = 312
37380 deg
ZDOT = 2983
739724 TA = 246
58683
MA = 246
62203
Ha = 188
659 n
mi
Hp = 184
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1463844
18 X = -369010
34
Y = -16130080
27 feet Y = -4921005
56 meter
Z = -14965937
51 Z = -4563598
81
XDOT = 20561
347014 XDOT = 6289
418584
YDOT = -10938
049068 feet/sec YDOT = -3263
710841 meter/sec
ZDOT = 9789
172324 ZDOT = 3014
239139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15440651
66 X = -4706310
63
Y = 4865035
26 feet Y = 1482862
75 meter
Z = -14973954
82 Z = -4564061
43
XDOT = -14794
121853 XDOT = -4509
248341
YDOT = -16498
269964 feet/sec YDOT = -5028
672685 meter/sec
ZDOT = 9906
357991 ZDOT = 3019
457916
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08181
52557395
00020000 00000-0 20000-3 0 9109
2 25544 51
6392 312
9159 0008926 308
4304 51
6058 15
74869047 30475
Satellite: ISS
Catalog Number: 25544
Epoch time: 08181
52557395 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 312
9159 deg
Eccentricity:
0008926
Arg of perigee: 308
4304 deg
Mean anomaly: 51
6058 deg
Mean motion: 15
74869047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3047
Checksum: 306
Coasting Arc #12 (Orbit 3062)
---------------------------------------
Vector Time (GMT): 2008/182/12:21:36
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5237481
68 A = 6725952
90 meter
Y = 3090533
37 meter E =
0004804
Z = -2876660
89 I = 51
38737
XDOT = -647
021972 Wp = 329
62759
YDOT = -5787
620718 meter/sec RA = 307
25934 deg
ZDOT = -5032
151285 TA = 243
55031
MA = 243
59960
Ha = 188
849 n
mi
Hp = 184
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17183338
83 X = -5257676
88
Y = 10139545
18 feet Y = 3031852
57 meter
Z = -9437863
81 Z = -2902153
10
XDOT = -2122
775500 XDOT = -557
810385
YDOT = -18988
256950 feet/sec YDOT = -5794
356178 meter/sec
ZDOT = -16509
682693 ZDOT = -5035
079108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13880418
22 X = 4230751
47
Y = 14267214
79 feet Y = 4348647
07 meter
Z = -9535793
38 Z = -2906509
82
XDOT = -16939
716583 XDOT = -5163
225615
YDOT = 5421
224865 feet/sec YDOT = 1652
389339 meter/sec
ZDOT = -16521
413903 ZDOT = -5035
726958
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 08182
54083658
00020000 00000-0 20000-3 0 9119
2 25544 51
6395 307
6944 0008932 312
6523 47
3887 15
74896635 30631
Satellite: ISS
Catalog Number: 25544
Epoch time: 08182
54083658 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 307
6944 deg
Eccentricity:
0008932
Arg of perigee: 312
6523 deg
Mean anomaly: 47
3887 deg
Mean motion: 15
74896635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3063
Checksum: 322
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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